GB1417614A - Power plant - Google Patents

Power plant

Info

Publication number
GB1417614A
GB1417614A GB1475473A GB1475473A GB1417614A GB 1417614 A GB1417614 A GB 1417614A GB 1475473 A GB1475473 A GB 1475473A GB 1475473 A GB1475473 A GB 1475473A GB 1417614 A GB1417614 A GB 1417614A
Authority
GB
United Kingdom
Prior art keywords
hydrogen peroxide
valves
motor
gas turbine
fuel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1475473A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP3280872A external-priority patent/JPS4899509A/ja
Priority claimed from JP4166972A external-priority patent/JPS491926A/ja
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Publication of GB1417614A publication Critical patent/GB1417614A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

1417614 Gas turbine engines NISSAN MOTOR CO Ltd 27 March 1973 [1 April 1972 25 April 1972] 14754/73 Heading FIG A gas turbine engine comprises a casing 14 internally divided by a catalyst 22 to form a feed chamber receiving hydrogen peroxide, and a combustion chamber 20 into which the steam and oxygen formed by exothermic catalytic decomposition of the hydrogen peroxide is fed to combust with liquid fuel 32 fed via a nozzle 34a, the combustion products then being directed against the blading 52 of the turbine. As shown, the combustion products pass through a Venturi portion 48 into flow passages 50, and cooling air is drawn into the hot gases through an inlet 56 in the Venturi portion. Turbines 30, 42 driven by the decomposition products of the hydrogen peroxide drive pumps 24, 36 feeding the hydrogen peroxide and fuel respectively. Valves 16, 46 controlling the supply of hydrogen peroxide and the venting of the decomposition products respectively, are themselves controlled in response to torque demand. Again, Fig. 2 (not shown), the air nozzle 56 and fuel pump 36 together with its associated parts are omitted, and a throttle valve (66) controls the fuel feed. Also, an energy storing flywheel (70) is coupled to the engine through a centrifugal clutch (74). A speed sensor on the flywheel shaft controls valves 16 and (66) to close the valves when the speed exceeds a predetermined value. The flywheel drives a vehicle multi-speed transmission (88) through a fluid coupling (86). In Fig. 3 (not shown), the flywheel shaft drives an electric generator (98) connected to an electric motor (104) driving the vehicle wheels. A battery (108) is connected to the motor and the generator to store excess electrical energy and to provide additional energy for the motor during vehicle acceleration. The gas turbine engine may alternatively be utilized in driving ships, aircraft, external electrical generators, emergency electrical power sources and/or portable electrical generators.
GB1475473A 1972-04-01 1973-03-27 Power plant Expired GB1417614A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP3280872A JPS4899509A (en) 1972-04-01 1972-04-01
JP4166972A JPS491926A (en) 1972-04-25 1972-04-25

Publications (1)

Publication Number Publication Date
GB1417614A true GB1417614A (en) 1975-12-10

Family

ID=26371390

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1475473A Expired GB1417614A (en) 1972-04-01 1973-03-27 Power plant

Country Status (3)

Country Link
US (1) US3898794A (en)
FR (1) FR2179019B1 (en)
GB (1) GB1417614A (en)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS51145504A (en) * 1975-05-28 1976-12-14 Nissan Motor Co Ltd A reformer
US4047380A (en) * 1976-04-09 1977-09-13 The United States Of America As Represented By The Secretary Of The Navy Combustion system using dilute hydrogen peroxide
US4135361A (en) * 1976-10-26 1979-01-23 The Charles Stark Draper Laboratory, Inc. Self-contained heat generating system
EP0144094B1 (en) * 1983-12-07 1988-10-19 Kabushiki Kaisha Toshiba Nitrogen oxides decreasing combustion method
US4759178A (en) * 1987-03-17 1988-07-26 Williams International Corporation Aircraft auxiliary power unit
JP2759748B2 (en) * 1993-11-20 1998-05-28 川崎重工業株式会社 High temperature and high pressure gas generator for turbine drive
FR2728627B1 (en) * 1994-12-27 1997-03-14 Europ Propulsion TANK SELF-PRESSURIZATION
US6255009B1 (en) * 1998-03-28 2001-07-03 The United States Of America As Represented By The Secretary Of The Navy Combined cycle power generation using controlled hydrogen peroxide decomposition
FR2792060B1 (en) * 1999-04-06 2001-09-07 Air Jonction Tech PROCESS FOR PRODUCING STEAM FROM SUPERHEATED WATER, STEAM GENERATOR USING THE SAME AND ITS INDUSTRIAL APPLICATIONS
GB9917404D0 (en) * 1999-07-26 2000-08-23 Secr Defence Hydrogen peroxide based propulsion system
US6349787B1 (en) * 2000-05-08 2002-02-26 Farouk Dakhil Vehicle having a turbine engine and a flywheel powered by liquid nitrogen
US6661112B2 (en) * 2001-04-02 2003-12-09 Bravo Zulu International Fluid control system with automatic recovery feature
US6532741B2 (en) * 2001-06-29 2003-03-18 United Technologies Corporation Gas generator for producing adjustable flow
CN1659372B (en) 2002-04-11 2012-12-26 克尼尔维利科技有限公司 Water combustion technology-methods, processes, systems and apparatus for the combustion of hydrogen and oxygen
US20050066662A1 (en) * 2003-09-26 2005-03-31 Cronce Donald T. Using solids as peroxide source for fuel cell applications, process and product thereof
US20060174605A1 (en) * 2005-02-07 2006-08-10 Berry Benny L Berry zero hydrocarbons engine
US20070107433A1 (en) * 2005-11-15 2007-05-17 Berry Benny L Hybrid electric steam turbine automotive engine
US7966805B2 (en) * 2007-05-15 2011-06-28 Raytheon Company Hydroxyl amine based staged combustion hybrid rocket motor
US8205827B2 (en) * 2008-01-23 2012-06-26 Aurora Flight Sciences Corporation Hydrazine monopropellant decomposition air turboprop engine
EP2508498A1 (en) * 2011-04-09 2012-10-10 Eckhard Braun Solar fuel based on monergol hydrogen peroxide
US20120282558A1 (en) * 2011-05-05 2012-11-08 General Electric Company Combustor nozzle and method for supplying fuel to a combustor
RU2527010C2 (en) * 2012-08-24 2014-08-27 Федеральное государственное бюджетное учреждение науки Институт энергетических проблем химической физики Российской академии наук Gas turbine plant with water steam injection
RU2527007C2 (en) * 2012-08-24 2014-08-27 Федеральное государственное бюджетное учреждение науки Институт энергетических проблем химической физики Российской академии наук Gas turbine plant with supply of steam-fuel mixture
EA202091967A1 (en) 2014-08-15 2021-03-31 Глоубал Ойл Эор Системз, Лтд. HYDROGEN PEROXIDE STEAM GENERATOR FOR OIL FIELD APPLICATIONS
CN106704531A (en) * 2015-11-16 2017-05-24 熵零股份有限公司 Energy adjusting method
CN105841193B (en) 2016-05-18 2018-07-20 葛明龙 Two kinds of aerospace fanjets
DE102019001876B3 (en) 2019-03-15 2020-06-10 Tivadar Menyhart Method, device and system for operating internal combustion engines with a significantly increased pressure ratio and vehicle with this system
WO2021239186A1 (en) * 2020-05-25 2021-12-02 Nexth202 Gmbh Zwickau Steam-operated turbine system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450950A (en) * 1945-06-11 1948-10-12 Daniel And Florence Guggenheim Gas blast actuated auxiliary turbine for gas blast propelled craft
US2926492A (en) * 1951-01-17 1960-03-01 Bendix Aviat Corp Self contained power plant using liquid decomposed into gaseous products
GB763015A (en) * 1954-05-25 1956-12-05 Napier & Son Ltd Power gas producing apparatus especially for rocket type propulsion devices
US3229462A (en) * 1964-04-22 1966-01-18 Fatica Nicholas Propulsion system
US3581504A (en) * 1968-08-28 1971-06-01 Aerojet General Co Monopropellant turbo gas generator
US3740945A (en) * 1969-02-27 1973-06-26 Thiokol Chemical Corp Injector for rocket motors using high viscosity fuel

Also Published As

Publication number Publication date
FR2179019B1 (en) 1976-01-30
US3898794A (en) 1975-08-12
FR2179019A1 (en) 1973-11-16

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee